1–20 of 94 hits
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    Investigation of the Use of Vectored Thrust during Carrier Landings

    DAVID P. MILLER AND JAMES W. CLARK | AIAA | 1966

    Finite-Element Approach to Compressor Blade-to-Blade Cascade Analysis

    Wagdi G. Habashi / Ernest G. Dueck / David P. Kenny | AIAA | 1979

    Effects of Compression-Compression Fatigue Balanced Graphite/Epoxy Laminates with Holes

    James W. Mar / Michael J. Graves / David P. Maass | AIAA | 1981

    Prototype Testing of Magnetic Bearings

    Plant, David P. / Jayaraman, Chaitanya P. / Frommer, David A. et al. | AIAA | 1987

    Grid generation and adaptation for the direct simulation Monte Carlomethod

    OLYNICK, DAVID P. / HASSAN, H. A. / MOSS, JAMES N. | AIAA | 1989

    Monte Carlo simulation of re-entry flows using a bimodal vibration model

    OLYNICK, DAVID P. / HASSAN, H. A. / MOSS, JAMES N. | AIAA | 1990

    Monte Carlo simulation of vibrational relaxation in nitrogen

    OLYNICK, DAVID P. / HASSAN, H. A. / MOSS, JAMES N. | AIAA | 1992

    Monte Carlo simulation of nonequilibrium shock fronts

    OLYNICK, DAVID P. / MOSS, JAMES N. / HASSAN, H. A. | AIAA | 1992

    Fighter agility metrics, research and test

    LIEFER, RANDALL K. / VALASEK, JOHN / EGGOLD, DAVID P. et al. | AIAA | 1992

    New two-temperature dissociation model for reacting flows

    OLYNICK, DAVID P. / HASSAN, H. A. | AIAA | 1993

    Measurement and improvement of the lateral agility of the F-18

    Eggold, David P. / Valasek, John / Downing, David R. | AIAA | 1993

    Using a full potential solver for propulsion system exhaust simulation

    MELVIN, ROBIN G. / JOHNSON, FORRESTER T. / YOUNG, DAVID P. et al. | AIAA | 1993

    High-accuracy algorithms for computational aeroacoustics

    Lockard, David P. / Brentner, Kenneth S. / Atkins, H. L. | AIAA | 1995

    Tangential Injection from Overlaid Slots into a Supersonic Stream

    David P. Lewis / Joseph A. Schetz | AIAA | 1997

    Radiated Noise from Airfoils in Realistic Mean Flows

    David P. Lockard / Philip J. Morris | AIAA | 1998

    Wing-Tip Vortex Calculations Using a High-Accuracy Scheme

    David P. Lockard / Philip J. Morris | AIAA | 1998

    Scaling Effects in Sublaminate-Level Scaled Composite Laminates

    David P. Johnson / John Morton / Sotiris Kellas et al. | AIAA | 1998